Research Article
Optimization of Fuel Injection Control System of Two-Stroke Aeroengine of UAV
Table 6
Optimize calibration data of fuel injection parameter.
| α (°)/n (RPM) | 2500 | 3000 | 3500 | 4000 | 4500 | 5000 | 5500 | 6000 |
| 10 | 15.5 | 15 | 15.5 | 15.5 | 15.5 | 15.5 | 15.5 | 15.5 | 20 | 15 | 14 | 15.5 | 15.5 | 15.5 | 15.5 | 15.5 | 15.5 | 30 | 14.5 | 12.5 | 15 | 15 | 15.5 | 15.5 | 15.5 | 15.5 | 40 | 15 | 15.5 | 15 | 15.5 | 15.5 | 15 | 15.5 | 15.5 | 50 | 15.5 | 15.5 | 12.5 | 15 | 15.5 | 15.5 | 13 | 15.5 | 60 | 15 | 15.5 | 14.5 | 15.5 | 15.5 | 15.5 | 15 | 14.5 | 70 | 15 | 15.5 | 15.5 | 15.5 | 15 | 13.5 | 13.5 | 14 | 80 | 13.5 | 15 | 15 | 15 | 14 | 15 | 14.5 | 15.5 | 90 | 15.5 | 15.5 | 15.5 | 15.5 | 14.5 | 15.5 | 13.5 | 13.5 |
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